| [1] Fehse W. Automated rendezvous and docking of spacecraft. New York: Cambridge University Press, 2003: 218-279.[2] Stoll E, Letschnik J, Walter U, et al. On-orbit servicing. IEEE Robotics and Automation Magazine, 2009, 16(4): 29-33.[3] Alfriend K T, Vadali S R, Gurfil P, et al. Spacecraft formation flying: dynamics, control, and navigation. Kidlington: Butterworth-Heinemann, 2009: 83-122.[4] Lefferts E J, Markley F L, Shuster M D. Kalman filtering for spacecraft attitude estimation. Journal of Guidance, Control, and Dynamics, 1982, 5(5): 417-429.[5] Bar-Itzhack I Y, Oshman Y. Attitude determination from vector observations: quaternion estimation. IEEE Transactions on Aerospace and Electronic Systems, 1985, 21(1): 128-136.[6] Kim S G, Crassidis J L, Cheng Y, et al. Kalman filtering for relative spacecraft attitude and position estimation. Journal of Guidance, Control, and Dynamics, 2007, 30(1): 133-143.[7] Xiong K, Liu L D, Liu Y W. Regularized robust filter for spacecraft attitude determination. Chinese Journal of Aeronautics, 2011, 24(4): 467-475.[8] Yang J, Ji H X, Wei M K. Error analysis and application of a nonlinear filter. Acta Aeronautica et Astronautica Sinica, 2011, 32(8): 1469-1477.(in Chinese) 杨静, 冀红霞, 魏明坤. 一种非线性滤波器的误差分析及应用. 航空学报, 2011, 32(8): 1469-1477.[9] Wan E A, van der Merwe R. The unscented Kalman filter for nonlinear estimation. The IEEE 2000 Adaptive Systems for Signal Processing, Communications, and Control Symposium, 2000: 153-158.[10] Crassidis J L, Markley F L. Unscented filtering for spacecraft attitude estimation. Journal of Guidance, Control, and Dynamics, 2003, 26(4): 536-542.[11] Carmi A, Oshman Y. Fast particle filtering for attitude and angular-rate estimation from vector observations. Journal of Guidance, Control, and Dynamics, 2009, 32(1): 70-78.[12] Cheng Y, Crassidis J L. Particle filtering for attitude estimation using a minimal local-error representation. Journal of Guidance, Control, and Dynamics, 2010, 33(4): 1305-1310.[13] Arasaratnam I, Haykin S. Cubature Kalman filters. IEEE Transactions on Automatic Control, 2009, 54(6): 1254-1269.[14] Arasaratnam I, Haykin S, Hurd T R. Cubature Kalman filtering for continuous-discrete systems: theory and simulations. IEEE Transactions on Signal Processing, 2010, 58(10): 4977-4993.[15] Chen J Z, Yuan J P, Fang Q. Flight vehicle attitude determination using the modified Rodrigues parameters. Chinese Journal of Aeronautics, 2008, 21(5): 433-440.[16] Schaub H, Junkins J L. Stereographic orientation parameters for attitude dynamics: a generalization of the Rodrigues parameters. Journal of the Astronautical Sciences, 1996, 44(1): 1-19.[17] Crassidis J L, Junkins J L. Optimal estimation of dynamic systems. Boca Raton: Chapman & Hall, 2004: 419-433.[18] Shuster M D. A survey of attitude representations. Journal of the Astronautical Sciences, 1993, 41(4): 439-517.[19] Hurtado J E. Interior parameters, exterior parameters, and a Cayley-like transform. Journal of Guidance, Control, and Dynamics, 2009, 32(2): 653-657.[20] Crassidis J L, Markley F L. Attitude estimation using modified Rodrigues parameters. Proceedings of the American Astronautical Society F. Landis Markley Astronautics Symposium, 1996: 71-86.[21] Arulampalam M S, Ristic B, Gordon N, et al. Bearings-only tracking of manoeuvring targets using particle filters. EURASIP Journal on Applied Signal Processing, 2004, 2004(15): 2351-2365. |
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